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Wind Tunnel Wall Effects at Extreme Force CoefficientsWind tunnel wall effects for highly deflected wakes
Document ID
19680015961
Acquisition Source
Headquarters
Document Type
Technical Memorandum (TM)
Authors
Heyson, H. H. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1967
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-59742
Report Number: NASA-TM-X-59742
Meeting Information
Meeting: INTERN. CONGR. OF SUBSONIC AERON.
Location: NEW YORK
Start Date: April 3, 1967
End Date: April 6, 1967
Accession Number
68N25433
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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